N932DL

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 74,866 hrs · 55,828 cycles

FWD LAVATORY SMOKE DETECTION SYSTEM- SMOKE DETECTOR SOUNDED WITH NO EVIDENCE OF SMOKE OR ODORS. REMOVED AND REPLACED THE FWD LAV TRASH SMOKE DETECTOR.

Part: FIRE LOOP — MALFUNCTIONED (A LOOP) · airframe 74,267 hrs · 55,337 cycles

LEFT ENGINE FIRE LIGHT ILLUMINATED WITH AURAL WARNING DURING DESCENT. ACCOMPLISHED QRH PROCEDURE. ENGINE FIRE LIGHT REMAINED ON AFTER BOTH FIRE BOTTLE AGENTS USED. ENGINE SHUTDOWN AT 27,000 FT. ALL ENGINE INDICATIONS NORMAL BEFORE SHUTDOWN. LEFT ENGINE LOOP A TEST LAMP ON OVERHEAD PANEL AND LEFT ENGINE FIRE HANDLE BOTH ILLUMINATED AT GATE. WHEN LOOP SELECTOR SWITCHED TO BOTH OR B, THE FIRE ALARM SILENCES AND LIGHTS EXTINGUISHED. WHEN SWITCHED BACK TO A, FIRE ALARM SOUNDS AND LIGHTS ILLUMINATE. TROUBLESHOT THE A LOOP IAW AMM 26-11-00. SWAPPED FIRE DETECTION CONTROL UNIT WITH RIGHT SIDE AND FAULT CLEARED. RETURNED TO ORIGINAL CONFIGURATION AND REPLACED LEFT FIRE DETECTOR CONTROL UNIT IAW AMM 26-10. LEFT FIRE DETECTION SYSTEM A TESTED GOOD.

Part: ENGINE — MAKING METAL (LEFT) · airframe 73,879 hrs · 55,019 cycles

LEFT ENGINE OIL STRAINER CLOGGED. EMERGENCY DECLARED. CHIP DETECTOR CLEAN AND FILTER CHECKED GOOD. FOUND METAL IN OIL TANK AND REPLACED ENGINE.

Part: CAP — DISPLACED (APU OIL SYSTEM) · airframe 73,820 hrs · 54,972 cycles

ON TAXI IN, CABIN BEGAN TO FILL WITH SMOKE. FOUND APU OIL CAP ON CROOKED AND OIL DRIPPING OUT OF APU INLET.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 73,070 hrs · 54,377 cycles

RIGHT HORIZONTAL STAB FRONT SPAR CAP HAD CRACK INDICATIONS, REPAIRED IAW ERA 556177-14 AD REV ORIG.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 73,070 hrs · 54,377 cycles

VERTICAL STABILIZER SPAR LEADING EDGE CRACKED. COMPLIED WITH ERA 556177-14AD, REV ORIG, AND PRIS 556177-14AD, REV 0-8.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 70,534 hrs · 52,539 cycles

MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 1 TO 30. THE BATTERY CHARGER AND DIODE WAS REPLACED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,450 hrs · 52,480 cycles

THE FLIGHT CREW OF FLIGHT 333, FOUND EMERGENCY EXIT LIGHTS AT LT AND RT FORWARD DOORS, FORWARD GALLEY, AND SEAT ROWS ROWS 1 THROUGH 30 INOPERATIVE. CVG MAINTENANCE REPLACED BATTERY PACK AND CHARGER B5-211 AND THE LIGHTS CHECKED OK.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,197 hrs · 52,308 cycles

CORROSION ON FUSELAGE SKIN AND INNER PRODUCTION DOUBLER AROUND AFT LAV SERVICE PANEL. ALSO CORROSION IS RUNNING UNDER SKIN, PANEL AND DOUBLERS. DUE TO EXCESSIVE CORROSION AREA WAS REPAIRED IAW ERA 541624-14, REV ORIG.

Part: SUPPORT BRACKET — CRACKED · airframe 70,197 hrs · 52,308 cycles

CRACKED UPPER BRACKET SUPPORT AND MISSING SCREW ON LOWER BRACKET SUPPORT OF EST NDAR ELECTRONIC MODULE AT FWD FACE OF FUEL CENTER TANK BRACKET SUPPORT WAS REPLACED IAW DWG 5939757-3, REV K.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 70,197 hrs · 52,308 cycles

CORROSION ON LOWER EDGE AT DOOR JAMB AFT, MID AND FWD CARGO. MID CARGO WAS ATTENDED WITH NRC 20000097097, CARD 156, ZONE 100, AFT CARGO: NEW SPACER WAS INSTALLED IAW ERA 489172-14, REV ORIGINAL SRM 51-10-3, PAR 21, 14, 38 AND 26 FWD CARGO WAS ATTENDED WITH NRC 20000098461, CARD 182, ZONE 100.

Part: SKIN — CORRODED (BS 674) · corrosion level 2 · airframe 70,197 hrs · 52,308 cycles

EXFOLIATION CORROSION BS 674 BETWEEN LONGERON 30 RT AND 29 RT AT FUSELAGE SKIN. REPAIR FUSELAGE SKIN AT BS 674 BETWEEN LONGERON 30 RT AND 29 RT WAS ACCOMPLISHED IAW ER/A 541626-14, REV ORIGINAL.

Part: ACCESS PANEL — DAMAGED (RUDDER) · airframe 70,197 hrs · 52,308 cycles

DAMAGE PAINT ON ACCESS PLATE 6508A, RUDDER. ACCESS PLATE 6508A, RUDDER WAS PAINTED IAW SRM 51-10-3B. PROCESS B & C AND METALIZED WAS REPAIRED IAW SRM 51-70-1A, D PAR 27.

Part: ACCESS PANEL — DAMAGED (NOT REPORTED) · airframe 70,197 hrs · 52,308 cycles

DAMAGE FLAME SPRAY ON ACCESS PLATE 6504A0. ACCESS PLATE 6504A WAS REPAIRED IAW SRM 51-70-1AD, PAR 23, AND CARD 2000-8149-01, JOB 000-002.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 70,197 hrs · 52,308 cycles

MAINTENANCE FOUND THE R1 EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE INDICATOR IN THE RED. THE R1 EMERGENCY ESCAPE SLIDE WAS REPLACED.

Part: SKIN — WORN (BS 1309) · airframe 70,197 hrs · 52,308 cycles

WEAR ON BS 1309, LONGERON 19R OUTER FUSELAGE SKIN. REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 3.

Part: LONGERON — CRACKED (BS 200) · airframe 70,197 hrs · 52,308 cycles

CRACKED LONGERON 4L AT INTERSECTION WITH FRAME AT BS 200. SECTION OF THE LONGERON WAS REMOVED IAW SRM 53-02, PAR 12, FIG 18. A NEW SECTION AND REPAIR SPLICE WERE ADJUSTED IAW SRM 53-02, PAR 12, FIG 18. THE NEW LONGERON AND SPLICE WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14 AND 21. NEW LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02, FIG 18.

Part: SKIN — DENTED (BS 168) · airframe 70,197 hrs · 52,308 cycles

PROTUBERANCE ON, BETWEEN LONGERON 24RT AND 25RT BS 168 AT OUTER FUSELAGE SKIN. THIS DAMAGE WAS FOUND WITH PREVIOUS REPAIR IAW SRM 53-04-2, FIG 2, SHEET 3.

Part: SKIN — CRACKED (BS 1480) · airframe 70,197 hrs · 52,308 cycles

CRACK ON FUSELAGE SKIN BS 1480. THE SKIN WAS REPAIR IAW SRM 53-01.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 70,185 hrs · 52,300 cycles

FWD CABIN, ROWS 30 AND UP, AISLE EMERGENCY LIGHTS INOPERATIVE, SEAT MOUNTED. REPLACED FUSE IN BATTERY PACK B5-211. OPS CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 70,173 hrs · 52,292 cycles

MAINTENANCE FOUND ALL AISLE AND L1 AND R1 EMERGENCY EXIT SIGNS INOPERATIVE. A WIRE FOR SEAT ROW 13-23 WAS FOUND DISCONNECTED AT PLUG AND COMING IN CONTACT WITH AIRFRAME. THE WIRE WAS REINSTALLED AND THE LIGHTS CHECKED OK.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 70,146 hrs · 52,271 cycles

MAINTENANCE FOUND EMERGENCY LIGHTING INOPERATIVE AFT OF SEAT ROW 35. THE BATTERY PACK FUSE WAS REPLACED AT ROW 35. LIGHTS CHECKED OK.

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 68,984 hrs · 51,405 cycles

DURING JACKSCREW INSPECTION FOUND RT VERTICAL STABILIZER STRUCTURE CRACKED. REMOVED RT VERTICAL STABILIZER SUPPORT ANGLE. THE SUPPORT ANGLE WAS FABRICATED, HEAT TREATED, DRILLED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04.

Part: SUPPORT — CRACKED (VERTICAL STAB) · airframe 68,984 hrs · 51,405 cycles

DURING JACKSCREW INSPECTION, FOUND LT VERTICAL SUPPORT STRUCTURE CRACKED. REMOVED LT VERTICAL STABILIZER SUPPORT STRUCTURE, CLIP, REPLACEMENT CLIP WAS FABRICATED. DRILLED, PAINTED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04 AS A REF.

Part: UNKNOWN — SMOKE (CABIN/COCKPIT) · airframe 68,668 hrs · 51,201 cycles

FLIGHT RETURNED TO DEPARTURE AFTER SMOKE ACCUMULATED IN THE CABIN AND COCKPIT. THE AFT LAVATORY SMOKE DETECTOR ALSO SOUNDED BRIEFLY. MAINTENANCE REPLACED A LEAKING APU AND ACCOMPLISHED THE PNEUMATIC SYS DUCT BURN OUT PROCEDURES.

Part: GASKET — LEAKING (APU OIL SYS) · airframe 68,630 hrs · 51,171 cycles

F/A AND PASSENGERS EXPERIENCED HAZE AND SMOKE IN CABIN AFTER TAKEOFF. THE AFT LAVATORY SMOKE DETECTOR WAS SOUNDING DURING THE CLIMB THROUGH 7000 FT. THE CREW DECLARED AN EMERGENCY AND RETURNED. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH OIL. A LEAK AT THE APU OIL SERVICE CAP WAS DETERMINED TO BE THE SOURCE OF THE INGESTED OIL. THE CAP GASKET WAS REPLACED AND A DUCT BURNOUT WAS ACCOMPLISHED. APU PLACED ON MEL FOR INLET DEEP CLEANING.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 66,671 hrs · 49,834 cycles

DURING INSPECTION OF THE L1 DOOR SLIDE, MAINTENANCE FOUND THE SLIDE PIN NOT ENGAGED AND SLIDE PARTIALLY INFLATED. MAINTENANCE R & R THE SLIDE PACK.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 65,670 hrs · 49,098 cycles

EMERGENCY ESCAPE LIGHT AT ROW 28 INOPERATIVE. FOUND WIRE BROKEN AT CONNECTOR. INSTALLED NEW CONNECTOR IAW CH 20, OPS CHECKED OK.

Part: CONDUIT — OUT OF POSITION (TAILCONE) · airframe 65,364 hrs · 48,883 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR THE CONDUIT .5. CLAMPS REPLACED AND CONDUIT ADJUSTED IAW THE MM.

Part: BRACKET — WORN (TAILCONE) · airframe 65,364 hrs · 48,883 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE LT AND RT SPRING BRACKETS ARE WORN BEYOND 50 PERCENT. BRACKETS REPLACED AND SYSTEM RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK COMPLETED SATISFACTORILY.

Part: SKIN — CRACKED (BS 1380) · airframe 65,364 hrs · 48,883 cycles

CRACK INDICATION ON SKIN ABOVE PYLON BS 1380, LONGERON 13L, ACCOMPLISHED HFEC OF AREA IAW NDT SPM 06-10-01, CRACK INDICATION VERIFIED. REMOVED CRACK COMPLETED, DAMAGE CONTAINED USING HFEC NDT 06-10-01-001.

Part: TURNBUCKLE — BROKEN (TAILCONE RELEASE) · airframe 64,149 hrs · 48,067 cycles

DURING INSPECTION, MX FOUND THAT THE TAILCONE CATWALK COUNTER BALANCE CABLE WAS BROKEN ON THE RT SIDE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE MOVEABLE CATWALK COUNTER BALANCE CABLE TURNBUCKLE WAS REPLACED AND THE OPS CHECK WAS GOOD.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,205 hrs · 47,425 cycles

DURING SERVICE CHECK, THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT ROW 35D. REPLACED SEAT 35D EMERGENCY LIGHT HARNESS CONNECTOR AND OPERATION CHECKED NORMALLY.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,525 hrs · 46,993 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN ABOVE ROW 23 WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 62,046 hrs · 46,658 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING BETWEEN SEAT ROWS 16 TO 30 WERE INOPERATIVE. MX FOUND A LOOSE CONNECTION AT THE BATTERY PACK AND SECURED. THE FUNCTIONAL CHECK OF THE SYSTEM WAS SATISFACTORY.

Part: LONGERON — CRACKED (BS 1437 L16L) · airframe 61,922 hrs · 46,576 cycles

DURING HMV, A CRACK WAS FOUND ON LT LONGERON 16 BS Y=1437. REPLACED LONGERON SECTION AND SPLICE IAW SRM 51-30-2 51-30-5 53-14-4 AND DWG 5910228, REV KH.

Part: LONGERON SPLICE — DAMAGED (BS 227 L2L) · airframe 61,922 hrs · 46,576 cycles

DURING HMV, ELONGATED HOLES WERE FOUND ON SPLICE AND LONGERON 2L STA Y=227 AT FUSELAGE INNER STRUCTURE. REPAIRED LONGERON AND SPLICE IAW SRM 53-02, FIG 18.

Part: SKIN — CORRODED (LT WING) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, CORROSION WAS FOUND ON LT WING LOWER SKIN AT STATION XRS=118 LENGTH 3.218" WIDE 0.531" AND DEPTH 0.054". AREA WAS BLENDED OUT AND LEAVE AS IS CONDITION IAW ER/A 506622-14 REV, ORIG.

Part: DOOR FRAME — WORN (FWD SERVICE DOOR) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, WEAR WAS FOUND ON FWD SERVICE DOOR FRAME FWD LOWER SECTION BS 172. REPLACED LOWER SERVICE DOOR FRAME IAW ER/A 506610-14 REV ORIG AND SRM 53-05 FIG 55.

Part: LONGERON — CRACKED (BS1437 L3L) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, CRACKS WERE FOUND ON LONGERON 3L BS 1437. REPAIRED LONGERON IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437 L3R) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 3R AT STA 1437. DAMAGE SECTION OF LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 463-465 L4R) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 4 RT BETWEEN BS 463 AND 465. LONGERON SECTION WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — CRACKED (BS 1429 L2-3R) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, CRACKS WERE FOUND ON FUSELAGE SKIN PRODUCTION. DOUBLER BS 1429 BTW LONGERON 2-3R AND BTW LONGERON 2-3L. REPLACED FUSELAGE SKIN PRODUCTION DOUBLER IAW DWG 5910011, REV CJ.

Part: SKIN — CRACKED (BS 195) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND ON FUSELAGE SKIN FWD SERVICE DOOR FRAME AREA AFT LOWER SECTION STA Y=195. CUT OUT DAMAGE SKIN AND INSTALL DOUBLER TRIPLER FILLED IAW ER/A 504401-14AD.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, CORROSION WAS FOUND ON PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT LOWER DOOR JAMB FROM STA Y=1160-1212. REPLACED REPAIR DOUBLER IAW ER/A 489172-14 REV ORIG AND SRM 53-05, FIG 123.

Part: LONGERON — WORN (BS 1409 L8L) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, WEAR WAS FOUND ON LT LONGERON NR 8 Y=1409. LONGERON WAS REPLACED BETWEEN STA Y=1402-1431 IAW SRM 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437 L12L) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 12L BS 1437. SECTION OF LONGERON WAS REMOVED BETWEEN BS 1446-1426 AND NEW SPLICE IN IAW SRM 53-02 PARA 12 FIG 18.

Part: LONGERON — CRACKED (BS1380) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND LONGERON 13R BS 1380. LONGERON REMOVED BS 1372-1401 AND NEW LONGERON SPLICED REPAIRED IAW SRM 53-02 FIG 18.

Part: SKIN — CRACKED (BS 323-404) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND ON FUSELAGE SKIN LOCATED ON FWD UPPER CORNER AT FWD CARGO COMPARTMENT DOOR CUTOUT BTW STA Y=374.5 AND LONGERONS 20-21 RT. DUE TO EXISTING REPAIR IN CLOSE PROXIMITY SKIN STA Y=323-404 AND BETWEEN LONGERON 18-22 RT WAS REMOVED AND REPAIRED IAW MD-88 SRM 53-04 FIG 12C AND ER/A 504395-14 REV ORIG.

Part: SKIN — DAMAGED (BS 788-807) · airframe 61,921 hrs · 46,575 cycles

DURING HMV SCRATCHES WERE FOUND AROUND RT WINDOW BELT FWD UPPER AND LOWER CORNERS. ALSO, AFT UPPER AND LOWER CORNERS BS 788-807. SRATCHES WERE BLENDED OUT AND REPAIRED IAW ER/A 504399-14 REV ORIG.

Part: SKIN — DAMAGED (BS 712-731) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, SCRATCHES WERE FOUND ON RT WINDOW BELT AFT EDGE UPPER CORNER BTW Y=712-731. AREA WAS BLENDED OUT AND REPAIRED IAW ERA 504399-14 REV ORIG.

Part: SKIN — DAMAGED (BS 769-788) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, SCRATCHES WERE FOUND AROUND RT WINDOW BELT FWD UPPER AND LOWER CORNERS ALSO AFT UPPER AND LOWER CORNERS STAY=769-788. AREA WAS BLENDED OUT AND REPAIRED IAW ERA 504393-14 REV ORIGAND ER/A 504399-14 REV ORIG.

Part: LONGERON — CRACKED (BS 1380 L11L) · airframe 61,921 hrs · 46,575 cycles

DURING HMV, A CRACK WAS FOUND ON LONGERON 11L BS 1380. REMOVED LONGERON AND INSTALLED NEW LONGERON AND SPLICE IAW SRM 53-02 FIG 18.

Part: SKIN — DAMAGED (BS 807-826) · airframe 61,921 hrs · 46,575 cycles

DURING HMV SCRATCHES WERE FOUND ON RT WINDOW BELT UPPER AFT CORNER BTW BS 807-826. BLENDED DAMAGE AREA AND REPAIRED IAW ER/A 504399-14 REV ORIG.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,834 hrs · 46,510 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN ROW 17D THROUGH 32D OF THE CABIN WAS INOPERATIVE. MAINTENANCE LAMPED LIGHTS AND REPLACED THE BATTERIES TO CORRECT THE REMAINING MALFUNCTIONS. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 61,505 hrs · 46,296 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 30 DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,792 hrs · 45,793 cycles

EMERGENCY PATHWAY LIGHTING IN THE FORWARD SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 160504007. (2012-D0156)

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN FLOOR MEMBRANE CORRODED STA 1140 LBL 54. INSTALLED REPAIR DOUBLER, FILLER, AND BRACKET PER EA 398191-14MA AND IDENTIFIED REPAIR PER PS 900-5-1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN FLOOR SUPPORT CHANNEL STA 200 LBL 12 CORRODED. REMOVED FLOOR SUPPORT, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW DC9/MD80 SRM 53-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN SEAT TRACK STA 200-256 HAS CORROSION RBL 22. INSTALLED NEW SECTION OF TRACK AND SPLICE AT STA 200-265 PER MD 80 SRM 53-05 FIG 4F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN FLOOR SEAT TRACK STA 1107 TO 1223 AREAS OF CORROSION LBL 44. INSTALLED SEAT TRACK AT 1107 TO 1223 LBL 44 PER SRM 51-30-5 PG 29.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

LEFT CABIN STA 1155-1174 LBL 45 - LBL 65 FLOOR CUSP AND GIRT LATCH ATTACH HAT FITTING HAVE CORROSION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN FLOOR ANGLE CORRODED STA 185 TO 195 LBL 53. INSTALLED FLOOR SUPPORT ANGLE AT STA 185 TO 195, LBL 53 PER MD88 SRM 51-30-1 PG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN FLOOR SUPPORT ANGLE HAS CORROSION STA 160 TO 200 RBL 42. REMOVED CORROSION ON FLOOR SUPPORT, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED FLOOR SUPPORT ANGLE PER DC-9/MD80 SRM 51-10-3 DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,215 hrs · 45,425 cycles

MAIN CABIN SEAT TRACK CORRODED STA 200-218 AND LBL 22 SAA 021 - CORROSION MAIN CABIN.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,046 hrs · 45,293 cycles

DURING LINE CHECK, MAINTENANCE FOUND FORWARD CABIN OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK BATTERIES FOR THE SAME PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD. AIRCRAFT IS OKAY FOR SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 59,842 hrs · 45,136 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS A SEAT 28D INOPERATIVE. MAINTENANCE RE-PINNED LIGHT CONNECTORS. OPERATION OF LIGHT NOW CHECKS OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 59,807 hrs · 45,114 cycles

DURING A SERVICE CHECK, MAINTENANCE FOUND THE FIRST CLASS EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 58,793 hrs · 44,381 cycles

AUTO PRESSURE CONTROLLER 1 & 2 FAILED AND ALL PAX OXYGEN MASKS DROPPED. CORR ACTION- BITE OF 1 & 2 PRESS CONTROLLERS FAULT AC MOTOR. RANG AND MEGGED WIRES FROM AC MOTOR TO AUTO PRESS CONTROLLERS. CKS GOOD. REPL OUTFLOW MOTOR AND ACTUATOR W/ NEW MOTORS INSTALLED IAW AMM 21-32-05-401. TESTS OK IAW AMM 31-32-00, PG 201.

Part: LANYARD — OUT OF POSITION (EVAC SLIDE) · airframe 58,641 hrs · 44,276 cycles

DURING LINE CHECK MAINTENANCE FOUND L2 DOOR SLIDE LANYARD INSTALLED IMPROPERLY. MAINTENANCE REPOSITIONED DOOR SLIDE LANYARD PER AMM.

Part: DOOR FRAME — CORRODED (BS 1155-1212) · airframe 58,254 hrs · 44,010 cycles

DURING PSV INITIAL INSP, THE AFT CARGO DOOR JAMB BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT STA 1155-1212. CORROSION WAS CONTAINED AND A REPAIR WAS INSTALLED IAW ER/A 489172-14, REV ORIG.

Part: WIRE — DAMAGED (CABIN) · airframe 57,973 hrs · 43,829 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE PER ECRM. OPERATION OF LIGHT NOW CHECKS GOOD. (2010-D1403) (DLM88103245)

Part: ENGINE — FAILED (NR 1) · airframe 57,475 hrs · 43,467 cycles

DURING CLIMB APPROACHING FL360, THE FLIGHT CREW REPORTED THAT THE NR 1 ENGINE "POPPED" AND THE EGT CLIMBED TO 800 DEGREES. FLIGHT CREW SECURED THE NR 1 ENG BY SHUTTING OFF THE FUEL FLOW AND DIVERTED THE ACFT TO A SAFE LANDING. CREW REMARKED THAT THEY DID NOT ENCOUNTER ANY BIRDS AFTER TAKEOFF. MX REPORTED METAL IN THE TAIL PIPE AND IS CURRENTLY REPLACING THE NR 1 ENGINE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,497 hrs · 42,769 cycles

CRACK INDICATION LOWER AFT CORNER OF FWD AIRSTAIR DOOR CUTOUT AND TOP TWO HOLES AT REPAIR DOUBLER DAMAGED AND EGG SHAPED IN OUTER SKIN NRC 104 & NRC 112.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 56,427 hrs · 42,718 cycles

EMERGENCY PATH LIGHT AT AFT F/A SEAT INOP AND AT 34DE. C/A: REPLACED QUICK DISCONNECT CONNECTOR AT AFT FLT ATTEN OP NORMAL AND RELAMPED LT ASSY AT SEAT 34DE. OPS NML.

Part: LIGHT — BROKEN (AFT EXIT SIGN) · airframe 56,427 hrs · 42,718 cycles

MX FOUND THE EMERGENCY EXIT SIGN AT THE AFT F/A SEAT TO BE INOPERATIVE. MX FOUND A WIRE BROKEN AT THE CONNECTOR. MX RE-PINNED THE CONNECTOR. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 56,235 hrs · 42,603 cycles

SMOKE ODOR FOLLOWED BY FWD LAV SMOKE ALARM-NO EVIDENCE OF FIRE. FOUND APU INLET CONTAMINATED WITH HYDRAULIC FLUID-FOUND B NUT IN LEFT WHEELWELL UNDER SPOILER SHUTOFF LEAKING-TIGHTENED SAME-CLEANED A/C BELLY AND APU INLET- PERFORMED OPN 5090 ALTERNATE DUCT BURNOUT AND OPN 7904 COELESCER BAG CHANGE-ALL CHECKS GOOD.

Part: DOOR FRAME — CRACKED (OVERWING EXIT) · airframe 56,098 hrs · 42,511 cycles

CRACKED OVERWING FRAME IAW ER/A 09-460094-12.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,797 hrs · 42,296 cycles

EMERGENCY LIGHT INOP AT ROW 31DE TO 38DE. REPLACED CABIN EMER BATT CHARGER IAW MM. OP CKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,612 hrs · 42,178 cycles

EMERGENCY FLOOR LIGHTING INOP AT ROWS 31-38. REPLACED AFT POWER SUPPLY AND BATTERY - OPERATES NORMAL, REPLACED AFT PWR SUPPLY AND BATTERY. OPS CKS OK.

Part: DUCT — FAILED (NR 1 ENGINE) · airframe 51,084 hrs · 39,202 cycles

AFTER SELECTION CLIMB POWER GOT A FIRE LIGHT ON NR 1 ENGINE FOLLOWED BY A BELL, RETARDED ENG TO IDLE AND LIGHT WENT OUT. INSP AREA FOUND WIRING AROUND NOSE ANTI-ICE VALVE DAMAGED. FOUND DUCT BLOWN APART. REPLACED DUCT. AFT CLAMP SECURED, FWD LOOSE NEEDS MID CLAMP, CW 426246. INSTALLED MID CLAMP AND TIGHTENED FWD NUT. UPON FURTHER INSP FOUND LEFT IGV ANTI-ICE TUBE DAMAGED 417998. REPAIRED SEVEN DAMAGED WIRES GOING TO P1-808 AND P1-809 COWL ANTI-ICE VALVE AND LEFT ANTI-ICE VALVE. CHK GOOD PER M/M 943755. REPLACED ANTI-ICE DUCT. A/C RAN TAKEOFF POWER PER M/M. NO TROUBLE NOTED.

Part: MOTOR — MALFUNCTIONED · airframe 47,902 hrs · 37,170 cycles

C/W QRH, YOKE TRIM SW STOPPED RUNAWAY BUT WOULD NOT MOVE OPPOSITE. ALT TRIM WORKED AS ADVERTISED. LATER WHILE S+L HEARD TRIM MOTOR HORN, BUT TRIM NOT MOVING. INSPECTED SCREWJACK. NO METAL ON BOTTOM OR TOP OF ACME NUT RESET C/B AND STOP SW. RAN STAB FULL TRAVEL W YOKE SW AND HANDLE. T/S PER M/M 27-40-00 101- CHECKS OK. REPLACED RELAYS R20-18, R20-15, R20-16 PER M/M. REPLACED PRIM AND ALT TRIM MOTORS PER M/M. RAN STP AND RTS CHECKS BOTH 1 AND 2 DFGC OK FOR SERVICE. TRIM MOTOR D1775-1 SN 1050 COND PRECAUTIONARY.

Part: WIRE — BURNED (COCKPIT) · airframe 47,625 hrs · 36,993 cycles

DURING ROTATION ON TAKEOFF, HAD A FLASH OF LIGHT IN VINCINITY OF CAPT RUDDER PEDALS AREA. ONCE AIRBORNE FOLLOWING C/B'S POPPED PEDESTAL LIGHTS, FLT RECORDER AND RT ENG IGN. MTC IN PROGRESS, FOUND WIRE BUNDLE THAT RUNS UNDER CAPTS FEET HAS NUMEROUS WIRES BURNED THRU AND OTHERS FIRE DAMAGED. COMPLETED ALL REPAIRS A CHECKOUTS ON N/R CARD 001 278549.

Part: SKIN — DAMAGED (BS 617 L27R) · airframe 47,393 hrs · 36,827 cycles

EXISTING SKIN REPAIR INSTALLED PER 266909-14 DID NOT MATCH ER/A, FASTENERS OMITTED. REPAIR PARTS WERE REMOVED, ADDITIONAL DAMAGE CUTOUT, AND LARGER REPAIR WAS INSTALLED.

Part: SKIN — CRACKED (FS 522 L21L) · airframe 47,393 hrs · 36,827 cycles

FUSELAGE SKIN WAS FOUND DAMAGED WITH A DENT AND A CRACK REPAIRED PER 456699-14.

Part: SKIN — DENTED (BS 227 L15L) · airframe 47,393 hrs · 36,827 cycles

FUSELAGE SKIN WAS DENTED AT FS 227 AND L-15L._DENT INSPECTED AND ALLOWED AS IS IAW MFG APPROVAL.

Part: ODOR — DETECTED (A/C PACK) · airframe 44,132 hrs · 34,491 cycles

BURNING SMELL IN CABIN. PERFORMED DUCT BURNOUT. NO SMELLS NOTED.

Part: ACCESS DOOR — MISSING (NR 2 ENGINE) · airframe 43,102 hrs · 33,742 cycles

N 2 ENGINE MANUAL START ACCESS DOOR MISSING. REPLACED SAME.

Part: SWITCH — DEFECTIVE (NLG) · airframe 40,312 hrs · 31,834 cycles

AFTER T/O WHEN GEAR HANDLE WAS RAISED THE NOSE GEAR RED UNSAFE MSG ILLUMINATED. REPLACED S1-412 INTERLOCK SWITCH.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 39,578 hrs · 31,309 cycles

AFTER TAKE OFF LT GENERATOR FAILED. STARTED APU AND PUT THE APU GENERATOR ON LINE. APU GENERATOR KICKED OFF LINE WITH AN AC CROSSTIE LOCKOUT. DIVERTED REPLACED LT GENERATOR AND GCU.

Part: HOSE — DAMAGED (TAIL COMPARTMENT) · airframe 38,704 hrs · 30,704 cycles

RT HYDRAULIC SYSTEM QUANTITY LOST ON CLIMBOUT. GEAR MANUALLY EXTENDED. DOORS REMAINED OPEN DURING LANDING. FOUND RT ENGINE HYDRAULIC FLEX LINE TO FILTER MODULE LEAKING. REPLACED SAME. LEAK CHECKS GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,538 hrs · 30,584 cycles

THE FUSELAGE SKIN WAS DENTED AND PUNCTURED NEAR STRINGER 21L BETWEEN FS 110 & 170. THE DAMAGE WAS REMOVED WITH 3 CUTOUTS. TWO SMALL CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER THE MD-88 SRM. THE LARGEST, 16 X 5 INCH, CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 384404-14, REV A.

Part: BULKHEAD — GOUGED (FS 95) · airframe 38,538 hrs · 30,584 cycles

FUSELAGE / BULKHEAD / NLG WHEEL WELL / RH SIDEWALL / FS 94 :WEB REPAIR THE WEB OF THE RH NOSE LANDING GEAR WHEEL WELL BULKHEAD WAS GOUGED BY A GEAR STEARING ACTUTATOR DURING A GROUND TUG OPERATION. THE GOUGE WAS REMOVED WITH A CUTOUT IN THE BULKHEAD WEB AND REPAIRED WITH AN ALUMINUM AND TITANIUM REPAIR DOUBLER PER ER/A 384387-14, REV A.

Part: SKIN — DELAMINATED (ELEVATOR TAB) · airframe 37,991 hrs · 30,211 cycles

DURING OVERHAUL OF ELEVATOR GEARED TAB, SERVICE DAMAGE WAS FOUND WHICH WAS BEYOND THE SCOPE OF LOCAL REPAIR. THEREFORE A RESKIN OF THE PART WAS ACCOMPLISHED. REPAIR PER ERA 417690-14

Part: WIRE HARNESS — BURNED (A/C BAY) · airframe 36,250 hrs · 28,932 cycles

RIGHT PACK FAN POPS C/B. FOUND WIRE HARNESS BURNED THROUGH AND ARCED AGAINST AIRCRAFT STRUCTURE APPROXIMATELY 12 INCHES ABOVE THE RIGHT PACK FAN CONNECTOR.

Part: SCUFF PLATE — CRACKED (SERVICE DOOR)

IN CLIMB PASSING THRU FL 360, A LOUD NOISE AND VIBRATION STARTED. F/C GALLEY AREA WAS MOST EXCESSIVE. VIBRATION STOPPED IN DESCENT THRU FL 185. FOUND R1 DOOR SCUFF PLATE BENT AND CRACKED. REPLACED SAME.

Part: FLUSH MOTOR — FAILED (FWD LAVATORY)

ACRID ODOR ASSOCIATED WITH ELECTRICAL OVERHEAT DETECTED IN THE FWD PSG CABIN. SOURCE DETERMINED TO BE THE FWD LAV. PULLED THE 3 C/BS FOR THE FLUSH MOTOR. THE ODOR WENT AWAY. COLLAR, OK. BLOCKED OFF THE F/C LAV FWD THE FLUSH MOTOR TO MCO AND PLAC.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

NR 1 ENGINE COMPRESSOR STALL ON CLIMB STEADY STATE POWER. RETURNED TO RSW. MECHANIC FOUND METAL IN THE TAIL PIPE. ENGINE CHANGE IN PROGRESS.

Part: RELAY — FAILED (STAB TRIM)

STAB TRIM INOP AT 250 KTS. REPLACED R20-15/R20-16 PRI TRIM RLYS-STAB TRIM SW-STAB TRIM CBL SW. ALL AS PRECAUTION DUE TO HISTORY. CKS GOOD.

Part: SPRING — BROKEN (NLG)

AFTER TAKEOFF, HAD NOSE GEAR UNSAFE LIGHT WITH GEAR HANDLE UP. NOSE GEAR FAILED TO RETRACT INITIALLY, AFTER ABOUT 10 MIN NOSE GEAR DID FINALLY RETRACT WITH A LOUD BANG. FOUND THE RIGHT RETRACT SPRING ASSEMBLY BROKEN. REPLACED SPRING, OPERATION NORMAL.

Part: TAB SKIN — DELAMINATED (LT AILERON)

DURING SHOP INSPECTION, LEFT WING AILERON TAB INBD, OUTBD T/E CORNERS WERE FOUND TO BE DAMAGED. THESE DAMAGES WERE REPAIRABLE PER SRM 51-70-1A, REPAIR NR 18, PG 109. PATCHED BOTH CORNERS WITH A GRAPHITE PRECURED PATCH.